View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 44909U 19096E 25341.30683482 .00000019 00000-0 36771-4 0 9998
2 44909 82.5204 107.2185 0216853 232.8281 125.2847 12.79745875277802
| Epoch (UTC): | 07 December 2025 07:21:50 |
| Eccentricity: | 0.0216853 |
| inclination: | 82.5204° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 107.2185° |
| argument of perigee: | 232.8281° |
| revolutions per day: | 12.79745875 |
| mean anomaly at epoch: | 125.2847° |
| orbit number at epoch: | 27780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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